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Reexamining the Mission Architecture Decision of Project Apollo: A New Parametric Perspective
Transient Energy Response Analysis of Vibro-Acoustic Systems with Fuzzy Uncertainty
Probabilistic Launch Delay Models for Human Spaceflight Missions
Prediction of Acoustic Loads on a Launch Vehicle: Nonunique Source Allocation Method
Fluctuations of liquid fuel in tanks with oil recovery units
Integrated Guidance and Control Design for Orbit Injection Phase of Launch Vehicle
Adjusted Instantaneous Impact Point and New Flight Safety Decision Rule
Three-Degree-of-Freedom Hypersonic Reentry Trajectory Optimization Using an Advanced Indirect Method
Temporal Wind Pairs for Space Launch Vehicle Capability Assessment and Risk Mitigation
Random Vibration Environment Standard Deviation Variation Verification for Solid Rocket Motors
Improved Formulation for Predicting the Load Capacity of Marman Clamps
Onboard Real-Time Generation of Launch Vehicle Abort Orbits
Longitudinal Aerodynamics of a Winged Reentry Vehicle at Supersonic Speed
Effect of Freestream–Plume Interaction on Launch Vehicle Aerodynamics
Skylon Aerospace Plane and Its Aerodynamics and Plumes
Operational Methodology for Large-Scale Deployment of Nanosatellites into Low Earth Orbit
Time Domain Aero Control Structure Interaction Studies of Indian Reusable Launch Vehicle
Effects of Shear-Layer Reattachment on the Nozzles of a Launch Vehicle
Prediction of In-Flight Radio Frequency Attenuation by a Rocket Plume
Mach Hydrocarbon-Fueled Scramjet Flight Experiment: The HIFiRE Flight 2 Project
Dynamics Simulation of a Small Satellite with a Robotic Manipulator for Additive Manufacturing
Effects of Protuberances on Surface Loads on the Vega-C Launch Vehicle
Control of High-Temperature Impinging Jet Issued from Overexpanded Rocket Nozzle
Statistical Energy Analysis for the Vibro-Acoustic System with Interval Parameters
Profiles of quick access to the orbital station for modern spacecraft
Analytical Solution for Transient Thermal Response of an Insulated Structure
Compression Response of Fluted-Core Composite Panels
Integrating Model-Based Systems and Digital Engineering for Crewed Mars Mission Planning
Reusables vs. Expendables: to Low Earth Orbit (LEO) and Beyond
Vent Valve for Test Launch Vehicle of Korea Space Launch Vehicle II
Evolving Government Roles in an Increasingly Commercial Space Transportation Market
Fault-Tolerant Control for Launch Vehicle Actuator Based on Adaptive Control
Computations of Side Loads in a Thrust-Optimized Parabolic Nozzle During High-Altitude Testing
Software Infrastructure for an Autonomous Ground Vehicle
Combined Nonlinear Controller for a Controlled-Floating Space Robot
Effect of Aerospike on Unsteady Transonic Flow over a Blunt Body